PART I-DESCRIPTIVE
12. Trimming tabs
There are two sets, (30) and (33), of elevator and rudder
trimming tab handwheels, one set to the left of each seat.
They embody trim indicators and operate in the natural
plane and sense.
A servo tab is fitted to each aileron and may be adjusted
on the ground for trimming purposes.
13. Flaps control
(i) The flaps are pneumatically operated and controlled by
the selector lever (29) on the central throttle box. This
lever has three positions, UP, TAKE-OFF (maximum
lift position), and DOWN, the TAKE-OFF position being
gated.
(ii) The flaps position indicator (19) is on the right-hand side
of the instrument panel.
14. Wheel brakes
A brakes lever (40) is fitted on each control column spade
grip, and the brakes may be operated by either lever,
being locked on for parking by means of the small clamps
(32) on the forward side of each control column below the
spade grip. Pressure at each brake is shown by the lower
needles on the pneumatic supply pressure gauge (20). The
pressure with brakes fully applied, and rudder central,
should be 100 lb./sq. in. at each wheel.
ENGINE CONTROLS
15. Throttle and mixture controls
Two throttle levers are fitted, one (28) on the central
pedestal and a second (35) on the left-hand side of the
cockpit. Mixture control is automatic, a weak mixture
being obtained at throttle settings giving -2 lb./sq. in.
boost or less. A friction adjuster knob (5) on the left-hand
side of the central throttle box adjusts the friction for
both throttle levers.
16. R.p.m. control levers
Two levers (26) and (36) are fitted, one alongside each
throttle lever. They are set forward to INCREASE and
back to DECREASE r.p.m. and the governed range is
1,900 and 2,500 r.p.m.
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